A/Prof. Shannon Ryan

STAFF PROFILE

Position

Head, Defence CoLab

Faculty

Applied Artificial Intel Inst

Department

A2I2P

Campus

Geelong Waurn Ponds Campus

Publications

Filter by

2020

A penetration model for semi-infinite ultra-high molecular weight polyethylene composite

L Nguyen, S Ryan, A Orifici, S Cimpoeru

(2020), pp. 286-289, HVIS 2019 : Proceedings of the 15th Hypervelocity Impact Symposium, Destin, Florida, E1

conference
2011

Whipple shield performance in the shatter regime

S Ryan, M Bjorkman, E Christiansen

(2011), Vol. 38, pp. 504-510, International Journal of Impact Engineering, C1-1

journal article

A ballistic limit analysis programme for shielding against micrometeoroids and orbital debris

S Ryan, E Christiansen

(2011), Vol. 69, pp. 245-257, Acta Astronautica, C1-1

journal article
2010

Honeycomb vs. foam: Evaluating potential upgrades to ISS module shielding

S Ryan, T Hedman, E Christiansen

(2010), Vol. 67, pp. 818-825, Acta Astronautica, C1-1

journal article
2009

Theoretical prediction of dynamic composite material properties for hypervelocity impact simulations

S Ryan, M Wicklein, A Mouritz, W Riedel, F Schäfer, K Thoma

(2009), Vol. 36, pp. 899-912, International Journal of Impact Engineering, C1-1

journal article
2008

Ballistic limit equation for equipment placed behind satellite structure walls

F Schäfer, S Ryan, M Lambert, R Putzar

(2008), Vol. 35, pp. 1784-1791, International Journal of Impact Engineering, C1-1

journal article

Hypervelocity impact on CFRP: Testing, material modelling, and numerical simulation

M Wicklein, S Ryan, D White, R Clegg

(2008), Vol. 35, pp. 1861-1869, International Journal of Impact Engineering, C1-1

journal article

Structural vibrations induced by HVI - Application to the Gaïa spacecraft

J Vergniaud, M Guyot, M Lambert, F Schafer, S Ryan, S Hiermaier, E Taylor

(2008), Vol. 35, pp. 1836-1843, International Journal of Impact Engineering, C1-1

journal article

Characterizing the transient response of CFRP/Al HC spacecraft structures induced by space debris impact at hypervelocity

S Ryan, F Schäfer, M Guyot, S Hiermaier, M Lambert

(2008), Vol. 35, pp. 1756-1763, International Journal of Impact Engineering, C1-1

journal article

A ballistic limit equation for hypervelocity impacts on composite honeycomb sandwich panel satellite structures

S Ryan, F Schaefer, R Destefanis, M Lambert

(2008), Vol. 41, pp. 1152-1166, Advances in Space Research, C1-1

journal article
2006

Numerical simulation of hypervelocity impact on CFRP/Al HC SP spacecraft structures causing penetration and fragment ejection

S Ryan, F Schaefer, W Riedel

(2006), Vol. 33, pp. 703-712, International Journal of Impact Engineering, C1-1

journal article

Funded Projects at Deakin

Other Public Sector Funding

Physical Resilience Roadmap ¿ Orbital Debris and impact damage Gaps and Capability Analysis

A/Prof Shannon Ryan

  • 2021: $30,410

Development of Bayesian optimisation tools for accelerated design and discovery of non-magnetic structural damping alloys

A/Prof Shannon Ryan, A/Prof Santu Rana, Dr Stewart Greenhill, Dr Julian Berk

  • 2021: $10,000

Industry and Other Funding

A schema for recording and ranking ballistic test data

A/Prof Shannon Ryan

  • 2021: $15,000

Supervisions

No completed student supervisions to report